N216WR

Service difficulty reports · 301

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N216WR' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2023031601769Floor Panel · peelingAFT CABIN FLOOR PANEL 242TF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 TF; P/N 147A5810-94; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS728;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 242TF AND TO BE INSTALLED ON TTG8Q00GS728Feb 11, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023031601768Floor Panel · peelingAFT CABIN FLOOR PANEL 242RF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 RF; P/N147A5810-2; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS72C;[02] VERIFIED STEP 1.Feb 11, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023032001756Vapor Barrier · crackedRT BS 663 VAPOR BARRIER CRACK AT RBL 48<[01] PREPARED DAMAGED AREA FOR REPAIR; AND PERFORMED DRY OUT; FOUND NO WATER; AS PER B737 SRM 51-70-04-2R-10.;[02] VERIFIED STEP 1; OK TO INSTALL REPAIR.;[03] APPLIED REPAIR AT R\H ON VAPOR BARRIER PER B737SRM 51-70-04-2Feb 10, 2023 · N216WR · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023031601453Floor Panel · delaminatedCABIN FLOOR PANEL 232BF FWD SIDE DELAMINATED<[01] PREPARED FOR REPAIR CABIN FLOOR PANEL 232 BF; AS PER B 737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 232BF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473813 AFeb 9, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023031601449Floor Panel · delaminatedCABIN FLOOR PANEL 231BF SURFACE DELAMINATED<[01] RECEIVED NEW CABIN FLOOR PANEL 231 BF; P/N 141A5810-168; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GXTW0;[02] VERIFIED STEP 1.Feb 9, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023032000764Support Angle · crackedCENTER WING REAR SPAR VAPOR WEB RIGHT SIDE FRONT WALL ACCESS BY AC BAY SUPPORT ANGLE SIGNS OF CRACK DOR EV16<[01] PERFORMED HFEC ON UPPER SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC.23; SUPPORT HAS APROX. 0.625' CRACK. TOOL USED OLYMPUS NORTEC 600; B/C 166Feb 8, 2023 · N216WR · Boeing 7377H4 · Wing, Center BoxSDR SWAA2023032000773Floor Panel · delaminatedCABIN FLOOR PANEL 241FF FWD CORNER DELAMINATED<[01] PREPARED FOR REPAIR FLOOR PANEL 241 FF; AS PER B737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 241 FF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473815 AND PFeb 8, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023032000774Floor Panel · delaminatedCABIN FLOOR PANEL 242DF DELAMINATED<[01] MEASUREMENTS;[02] PREPARED DAMAGED AREA TO APPLY REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 53-00-50-2R-7;[03] VERIFIED STEPS 1 AND 2;[04] OK TO APPLY REPAIR;[05] APPLIED REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 5Feb 8, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023032000354Panel · crackedLH UNDERWING ACCESS PANEL 192HL LOWER SURFACE AROUND FASTENER HOLE HAS MATERIAL CRACKED.<[01] PREPARED FOR REPAIR PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9 MATEFeb 8, 2023 · N216WR · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023031600775Floor Panel · delaminatedCABIN FLOOR PANEL 231FF L/H AREA DELAMINATED FLOOR PANEL 231 FF<[01] PREPARED FOR REPAIR; FLOOR PANEL 221 FF; AS PER B737 SRM 53-00-50-2R-9;[02] CORRECTION #1. PREPARED FOR REPAIR FLOOR PANEL 231FF; AS PER B737 SRM 53-00-50-2R-9;[03] VERIFIED CORRECTED STEP 2.Feb 8, 2023 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023031601118Angle · crackedCENTER WING VAPOR WEB FWD WALL AREA ABOUT RBL10 SUPPORT ANGLE EVIDENCE OF CRACK<[01] PERFORMED A HFEC INSP. ON SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC. 23; 0.500' CRACK CONFIRMED. TOOL USED OLYMPUS NORTEC 600; B/C 172389; CAL DUE DATE 03/23.;[23] REMOVFeb 8, 2023 · N216WR · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023031600770Girt Bar · out of adjustR1 DOOR SLIDE GIRT NEEDS REPACK<[01] NON-ROUTINE WRITTEN IN ERROR. SHOULD READ R1 DOOR SLIDE SKIRT IS TOUCHING CABIN FLOOR. [TTG8Q00J0H2Y];[02] VERIFIED STEP 1Feb 8, 2023 · N216WR · Boeing 7377H4 · Escape SlideSDR SWAA2023032000353Panel · elongatedACCESS PANEL 661BB SEVERAL HOLES ENLONGATED<[01] PREPARED AREA FOR REAPAIR HOLES AT PANEL#661BB AS PER B737 SRM 51-70-04-2R-9;[02] REPAIRED DAMAGED AREA AT PANEL#661BB AS PER B737 SRM 51-70-04-2R-9 MATERIAL USED PO#1690463 PO#1800112;[03] VERIFIED STEPS 1 AND Feb 7, 2023 · N216WR · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022092283064Slide · out of positionFWD ENTRY DOOR SLIDE IS DIFFICULT TO ENGAGE AND DISENGAGE / [01] REPOSITIONED FWD ENTRY DOOR SLIDE GIRT BAR FLAP IAW AMM 25-66-01.Sep 19, 2022 · N216WR · Boeing 7377H4 · Escape SlideSDR SWAA2022081742699Girt Bar · out of positionFA REPORTS FRONT SERVICE DOOR ESCAPE SLIDE GURT BAR IS DIFFICULT TO PULL OUT OF THE HOOKS IN THE UNARMED (STORED) POSTION / [01] ADJUSTED GURT BAR CLIPS. OPS CKS GOOD PER MM 25-66-01Aug 16, 2022 · N216WR · Boeing 7377H4 · Escape SlideSDR SWAA2022081642357Slide · pulledPROVISIONING OPENED FORWARD SERVICE DOOR AND GURT BAR CAUGHT EDGE OF DOOR FRAME AND PARTIALLY PULLED ESCAPE SLIDE COVER OPEN. SLIDE DID NOT INFLATE. / [01] REPACKED FORWARD SERVICE DOOR SLIDE PER MM 25-66-01-400-804.Aug 15, 2022 · N216WR · Boeing 7377H4 · Escape SlideSDR SWAA2022032083234Light · inoperativeFOWARD SERVICE DOOR SLIDE LIGHT IS INOP / [01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR SLIDE LIGHT PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Mar 13, 2022 · N216WR · Boeing 737* · Emergency LightingSDR SWAA2022032080212Light · inoperativeL/H OVERWING ESCAPE GROUND ILLUMINATION LIGHT IS INOP L547 / [01] RELAMPED L/H OVERWING ESCAPE GROUND ILLUMINATION LIGHT L547 AND PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION 1. TEST GOOD.Mar 5, 2022 · N216WR · Boeing 737* · Emergency LightingSDR SWAA2022032080213Light · inoperativeBOTH L/H AND R/H OVERWING ESCAPE HATCH LIGHT ASSEMBLIES ARE INOP (L751) / [01] REPLACED LAMPS FOR L/H AND R/H OVERWING ESCAPE HATCH EMERGENCY EXIT LIGHTS AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 5, 2022 · N216WR · Boeing 737* · Emergency LightingSDR SWAA2022032080214Battery Pack · inoperativeALL EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP / [01] REPLACED BATTERY PACK M1673 AND PERFORMED GOOD TEST PER AMM 33-51-00-960-805.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 5, 2022 · N216WR · Boeing 737* · Emergency LightingSDR SWAA2022032176447Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE IS CRACKED / [01] WELDED CRACK ON RADIUS OF ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID; E10583. S/N; KJ256554;[02] VERIFIED FWD CORNER SCUFFeb 22, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032175520Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19L/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 L/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART# 143A9481-5; LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALLFeb 19, 2022 · N216WR · Boeing 737* · Fuselage Main, Plate/SkinSDR SWAA2022032175521Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19R/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 R/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART#143A9481-6; LOCATED AND DRILL IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALL;[0Feb 19, 2022 · N216WR · Boeing 737* · Fuselage Main, Plate/SkinSDR SWAA2022032174003Intercostal · crackedAFT CARGO BAY INTERCOSTAL CRACKED BS 946 LBL 25 WL 163 / [01] REMOVED INTERCOSTAL AT ACB AT BS 927 TO 947 RBL 25 WL 163 AND EVALUATED DAMAGE ON INTERCOSTAL NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM; WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-40-02 AND 51-10-02 Feb 18, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032173452Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE IN ACB BS 947 RBL 22.5; WL 179.8 / [01] REMOVED BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS 947 ;RBL 22.5 ; WL 179.8 AND EVALUATED DAMAGE BULKHEAD SUPPORT ANGLE NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM; Feb 17, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032171162Angle · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA 120.30) HAS CRACK AT FWD ATTACH ANGLE / [01] VERIFIED APPLICABILITY.<BR>REMOVED DAMAGED FWD ATTACH ANGLE AT RT HORIZONTAL STABILIZER RIB 4. IAW B737 SRM 51-40-02.;[02] EDITED REPAIR TYPE IN MEASUREMENT FIELD. ATTACH ANGFeb 11, 2022 · N216WR · Boeing 737* · Horizontal Stabilizer, Spar/RibSDR SWAA2022032170784Rib · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) HAS CRACK AT STIFFENER #4 LOWER RADIUS / [01] VERIFIED APPLICABILITY OF REPAIR MANUAL SRM 55-10-09-2R-5.<BR>REMOVED DAMAGED AT RT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) STIFFENER #4 LOWER RADIUS. IAW B737 SFeb 10, 2022 · N216WR · Boeing 737* · Horizontal Stabilizer, Spar/RibSDR SWAA2022032169450Floorboard · out of toleranceFAB NEW 232HF FLOOR BOARD / [01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 3 SECTION 43 .<BR>FLOOR PANEL 232HF BEYOND ECONOMICAL REPAIR PER SRM 53-00-50-1A-1 PARA 4 A-E . REPLACE FLOOR PANEL AS GIVEN IN SRM 53-00-50-2R-0 PARA 1 A NOTE.;[02] USING MATEFeb 6, 2022 · N216WR · Boeing 737* · Fuselage Floor PanelSDR SWAA2022032168800Rail · corrodedACB FLOOR RAIL RBL3. HAS VISIBLE TWIST BETWEEN BS767 AND BS787 / [01] SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE FOR THIS AIRCRAFT.;[02] DAMAGE TO RAIL FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2.;[03] REMOVED DAMAGED PART OF RAIL IAFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168798Rail · corrodedACB FLOOR RAIL CORRODED AT BS767+5'; RBL3 / [01] REMOVED CORROSION ON ACB FLOOR RAIL AT BS 767+5 RBL 3 IN AREA OF L=1' X W=3' D=.008' REMAINING THICKNESS =.055' FROM ORIGINAL THICKNESS .063' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-01-2; SRM 53-00-53-1A-2 B Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Main, Floor BeamSDR SWAA2022032169067Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS847+8 RBL22. / [01] CORROSION ON SHIELD IS OUT OF LIMITS DUE TO NO ARE GIVEN SRM AT ACB BS 847+8' RBL 22 WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR. 9.;[02] RECEIVED NEW SHIELD P/N 146A8127Y10ATSMRO ; LOT: 1Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169069Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AROUND FASTENER HOLES AT AFT CARGO BAY BS887 BL0 / [01] ACB FLOOR SPLICE BS887; FOUND THERE ARE NO ALLOWABLE DAMAGE LIMITS PER SRM. REPAIR BY REPLACEMENT OF PART;[02] EDITED DAMAGE CHART;[03] REMOVED ACB FLOOR SPLICE AT BS887 Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169071Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS887+2; BS927+8 RBL13. / [01] REMOVED CORROSION ON TRACK AT AFT CARGO BAY BS 887+2; RBL 13; WORK AREA L 1.0'X W 1.0'X D 0.024'; BS 927+8; RBL 13; WORK AREA L 1.0'X W 1.0'X D 0.021 ; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-5Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169073Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS947 LBL9 TO RBL13. / [01] REMOVED CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS 947 LBL9 TO RBL13 IAW SRM 51-10-HOLE NOT DRILLED AND SEVERAL HOLES NOT COUNTERSUNK. SEE SFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169077None · corrodedCORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS987 S-22L. MARKED. / [01] EVALUATED STRINGER CLIP AT AREA AFT OF ACB BS987 S-22L. AND NOT FOUND ALLOWABLE DAMAGE LIMITS ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED STRINGER CLIP AT AREA AFT OF ACFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Main, Longeron/StringerSDR SWAA2022032169076Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS866 S-18R. MARKED. / [01] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 866 S-18R IAW SRM 51-10-02 PARAGRAPH 15 ;EVALUATED DAMAGE ;REWORKED AREA ;THE DEPPEST AREA BS 866 STR 18R; DIMENSION L=3' ;W=2' DEPTH=0.012' ORIGINAL THIFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Main, StructureSDR SWAA2022032168809Intercostal · corrodedLOWER DOOR SURROUND STUCTURE INTERCOSTAL CORROSION LOWER SURFACE COMMON TO NUT PLATES. RBL19.5; BS807-3'; BS807+2'; BS807+5.75'; BS807+9.5'; BS807+13'; BS807+16.75'; BS827+4'; BS827+7.5'; BS827+11.25' / [01] SRM 53-60-15-1A-1 IS FOUND TO BE APPLICABLE;[02] REMFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168780Track · crackedACB TRACK CRACKED IN RADIUS; BS767; RBL13.84 / [01] ACB TRACK IN RADIUS AT BS 767;RBL 13.84 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[10] INSTALLED NEW CARGO TRACK BTW B/S 747+10' TO B/S 887 RBL 13.84 ; IAW SRM 51-40-02 AND DWG 146A7500 REV:A;[11] VERIFFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169065Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL10. / [01] REMOVED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS918 RBL10 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW STIFFENER AT ACB BS918 RBL10 IAW SRM 51-40-05 AND BOEING DWG 147A722Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032169072Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL10. / [01] REMOVED STIFFENER BEHIND WATER SERVICE PANEL ACB BS 914 RBL10 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW STIFFENER AT ACB BS914 RBL 10 IAW SRM 51-40-05 AND BOEING DWG 147A7221Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168772Support · corrodedCORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT FROM STA 400+1 TO STA 500B+18; LBL 24; WL 156. / [01] BLENDED ALL CORROSION FROM STA 400+1 TO STA 500B+18 LBL24 IAW SRM 51-10-02-0G-0G<BR><BR>STA 400+6' : 0.002' <BR>STA 400+10' : 0.003'<BR>STA 400+18' : 0.002'<BRFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168773Support · corrodedCORROSION ON FCB AFT BULKHEAD SUPPORT FROM RBL 24 TO LBL 24; STA 500D; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS FOR FCB AFT BULKHEAD CTR SUPPORT ANGLE PER SRM. REPAIR BY REPLACEMENT OF PART;[02] REMOVED FCB AFT BULKHEAD CTR SUPPORT ANGLE PER SRM 51-40-02;[03]Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168775Shield · corrodedCORROSION ON FCB DOOR CUT-OUT FWD SHIELD FROM STA 420 TO 440; RBL 24; WL 156. / [01] NO ENTRIES FOR ALLOWABLE DAMAGE ON SRM FOR THIS ITEM; REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR. 9.;[02] LOCATED AND DRILLED NEW FCB DOOR CUT-OUT FWD. SHIELD BS420 - BSFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168768Support · corrodedCORROSION ON FCB R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO STA 500D; RBL 24; WL 156. / [01] SRM 3-00-53-1A-2 IS APPLICABLE<BR><BR>REMOVED CORROSION FROM 16EA. LOCATIONS AT FCB R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO STA 500D; RBL 24; WL 156. IAW SRFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168769Shield · corrodedCORROSION ON FCB DOOR CUT-OUT AFT SHIELD FROM STA 480+14 TO STA 500A; RBL 24; WL 156. / [01] NO ENTRIES FOR ALLOWABLE DAMAGE ON SRM FOR THIS ITEM; REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR. 9;[02] LOCATED AND DRILLED NEW FCB CUT-OUT DOOR AFT SHIELD FROMFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168774Web · corrodedCORROSION ON FCB DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 460 TO STA 480+4; RBL 28; WL 156. / [01] REMOVED CORROSION ON FCB DOOR CUT-OUT SUB-THRESHOLD WEB AT AREA 1 BS460 RBL 28 L=1' X W=1' D= 0.009' REMAINING THICKNESS = 0.036 FROM ORIGINAL THICKNESS= 0.45'. AFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168791Intercostal · corrodedACB INTERCOSTAL AT BS767-BS787 CORRODED TOP AND I/B SURFACES. RBL20; BS767+4.5' TO 7'; BS767+18' / [01] REMOVED CORROSION FROM ACB INTERCOSTAL AT BS767-787 RBL20 MEASURED 3.3'L X 1.9'W AND 0.007' DEEP; ORIGINAL THICKNESS OF 0.063' FOUND OUT OF LIMITS PER SRM 5Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168782Angle · corrodedACB LOWER DOOR SURROUND STRUCTURE; ANGLE COMMON TO FWD SHIELD AND INTERCOSTAL CORRODED. BS787+1.25' TO BS787+2.25'; RBL20.5; WL157 / [01] REMOVED CORROSION ACB LOWER DOOR SURROUND STRUCTURE ;ANGLE COMMON BS 787+1.25' TO BS 787+2.25' RBL 20.05 WL 157;DIMENSION Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032185761Intercostal · corrodedACB LOWER DOOR SURROUND STRUCTURE; ANGLE COMMON TO FWD SHIELD AND INTERCOSTAL CORRODED. BS787+1.25' TO BS787+2.25'; RBL20.5; WL157 / [01] REMOVED CORROSION ACB LOWER DOOR SURROUND STRUCTURE ;ANGLE COMMON BS 787+1.25' TO BS 787+2.25' RBL 20.05 WL 157;DIMENSION Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168785Support · corrodedACB RH FLOOR TO SIDEWALL SUPPORT CORRODED. RBL21; BS747; BS747+5.5'; BS747+8.5'; BS747+10.5'; BS747+14.5'; BS747+15'; BS747+18.5'; BS767. / [01] REMOVED CORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT RBL 21 ; WORK AREAS BS 747; L 1.0'X W 1.0'; D 0.014'; BS 747+Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous Structure
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